SAE Papers

Paper Number	Paper Title	Book Number
1999-01-1408	Micromachined Heat Sinks
981814	A Capillary Pump Loop Cooling System for the Nicmos Instrument
981543	Application of Mil-C-87252 in F-22 Liquid Cooling System
951400	Integrated Environmental Control System and Liquid Cooling System for F/A-18 E/F Aircraft
942176	Test Results of Reflux-Cooled Electromechanical Actuator
942177	Venturi-Flow Cooling System: Comparison of Numerical and Experimental Results
932120	A Centrifugal Pump Concept Designed for Multiple Use in Space
932119	A Low Fin Height Heat Exchanger Technology Demonstrator for Hermes
932122	A Thermal Method for the Determination of Solar Absorptance and Thermal Emittance of Spacecraft Coatings
932306	Computer Model of Satellite Thermal Control System Using a Controlled Capillary Pumped Loop
932239	Cphts Hardware Development for the Eos Am Spacecraft Instruments
932302	Design and Test of a Honeycomb Radiator Panel With Carbon Fiber Reinforced Plastic Facesheets and Aluminum Heat Pipes
932234	Eos Am Capillary Pumped Heat Transport System Development Testing Using Tdm
932305	Experimental and Theoretical Investigation of Startup Regimes of Two-Phase Capillary Pumped Loops
932236	Flow Visualization Within a Capillary Evaporator
932085	Global Research, Global Power, a Goal Denied?
932303	High Capacity Grooved Heat Pipes
932084	High Heat Sink Fuels for Improved Aircraft Thermal Management
932086	Improving Aircraft Fuel-Thermal Management
932301	In-Orbit Demonstration of Two-Phase Heat Transport Technology: Tpx/G557 Development and Pre-Launch Testing
932304	Investigation of the Heat Transfer Performance of a Capillary Pumped Ammonia Loop Under Gravity
932116	Porous Insulation Performance Under Martian Environment
932118	Sorption Refrigerants--A Review of Current Development Status
932117	Survey and Evaluation of Multilayer Insulation Heat Transfer Measurements
932121	Technology Improvements to Optical Solar Reflectors
932235	Testing of Flight Components for the Capillary Pumped Loop Flight Experiment
932307	The Experience of Finite Elements Method Utilization for Simulation of Heat-Mass Transfer in Heat Pipes and Other Elements of Thermal Control Systems
932123	Thermal Control Coatings on Mg-Li Alloys
932237	Thermal Control Subsystem Design for the Eos Thermal Infrared Radiometer
931397	Advanced Passive Cooling for High Power Electromechanical Actuators
921941	A Thermal Management Assessment Tool for Advanced Hypersonic Aircraft
921944	Arterial Heat Pipe Performance in a Transient Heat Flux and Body Force Environment
921942	Evaluation of Cooling Concepts for High Power Avionics Applications
921943	Heat Transfer in Two-Dimensional Jet Impingement of a Dielectric Liquid on to a Flat Plate With Uniform Het Flux
900965	Heating/Cooling With Polymeric Heat Exchangers
892316	Closed-System, High-Flux Evaporative Spray Cooling
871801	Flight Test Results for Several Light, Canard-Configured Airplanes
861724	Magnetic Refrigeration for Space Platforms
851856	Active Control of Compressible Flows on a Curved Surface
840940	The Closed-Loop Air-Cycle Option for Equipment Cooling on Aircraft
811083	High Speed Vscf Generator Design Consideration
801131	The All-Electric Airplane as An Energy Efficient Transport
670838	Design and Transient Performance of a Space Vehicle Liquid Coolant System
660208	Application of Vapor-Cycle Cooling Systems to Business Aircraft
650308	Analytical and Experimental Study of Vortex Subcooler--A New Concept in Mass Transfer Cooling
610437	Cooling for hypersonic aircraft structures